FIELD: engines and pumps.
SUBSTANCE: low-thrust rocket engine consisting of a motor head, a fuel spark plug, a system for supplying fuel components to an electrospark discharge zone, and to an internal combustion chamber cooling. In the combustion chamber, a centrifugal hydrogen nozzle and at least six peripheral jet oxygen nozzles are installed with the possibility of active interaction of the hydrogen flow and oxygen jets. The nozzles are arranged evenly around the circumference on the surface of the head, and the axes of which are directed at an angle of 35°-45° to the axis of the engine.
EFFECT: increased combustion efficiency of gaseous hydrogen and oxygen and reliability of the engine operation.
1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| LOW-THRUST ROCKET ENGINE ON NON-SELF-INFLAMMABLE LIQUID FUEL AND GASEOUS OXIDANT | 2019 |
|
RU2724069C1 |
| IGNITION DEVICE FOR LOW-THRUST ROCKET ENGINES ON NON-SELF-IGNITING GASEOUS (LIQUID) FUEL AND GASEOUS OXIDIZER | 2020 |
|
RU2778416C2 |
| HYDROGEN-OXYGEN LOW THRUST ENGINE | 2016 |
|
RU2623610C1 |
| THRUSTER AT GASEOUS HYDROGEN AND OXYGEN WITH CENTRIFUGAL NOZZLES | 2016 |
|
RU2628143C1 |
| LOW-THRUST ROCKET ENGINE ON GASEOUS HYDROGEN AND OXYGEN WITH JET-TYPE INJECTORS IN AIR CROSS-FLOW | 2017 |
|
RU2641785C1 |
| THRUSTER (RDMT) CHAMBER WORKING ON TWO-COMPONENT ANERGOLIC GASEOUS FUEL (VERSIONS) | 2008 |
|
RU2369766C1 |
| GASEOUS HYDROGEN AND OXYGEN THRUSTER WITH SLOT NOZZLE | 2016 |
|
RU2624419C1 |
| METHOD OF LOW-THRUST ROCKET ENGINE CHAMBER OPERATION | 2011 |
|
RU2477383C1 |
| CHAMBER OF LOW-THRUST ROCKET ENGINE RUNNING ON TWO-COMPONENT ANERGOLIC GAS FUEL | 2011 |
|
RU2448268C1 |
| CHAMBER OF LIQUID-PROPELLANT ROCKET ENGINE OR GAS GENERATOR WITH LASER IGNITION DEVICE OF FUEL COMPONENTS, AND ITS STARTUP METHOD | 2011 |
|
RU2468240C1 |
